| FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) |   | 96% | | 90% | 2 | 14 | 2 | 52 | 0 | 1 |
| addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) | | 95% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
| computeJacobianMeanWrtCartesianElliptical() | | 100% | | n/a | 0 | 1 | 0 | 86 | 0 | 1 |
| computeJacobianMeanWrtCartesianHyperbolic() | | 100% | | n/a | 0 | 1 | 0 | 89 | 0 | 1 |
| FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean) | | 100% | | 100% | 0 | 4 | 0 | 60 | 0 | 1 |
| computePVWithoutA() | | 100% | | 100% | 0 | 3 | 0 | 28 | 0 | 1 |
| nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
| FieldKeplerianOrbit(Field, KeplerianOrbit) | | 100% | | 100% | 0 | 7 | 0 | 11 | 0 | 1 |
| initPosition() | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
| shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 17 | 0 | 1 |
| referenceAxes() | | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
| computeJacobianTrueWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
| computeJacobianTrueWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
| toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| computeJacobianEccentricWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
| computeJacobianEccentricWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| toString() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| getHxDot() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| getHyDot() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getEccentricAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getMeanAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| getEquinoctialExDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getEquinoctialEyDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| checkParameterRangeInclusive(String, double, double, double) | | 100% | | 75% | 1 | 3 | 0 | 4 | 0 | 1 |
| getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| removeRates() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getEccentricAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getMeanAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getLvDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getAnomaly(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getAnomalyDot(PositionAngleType) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
| getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldKeplerianOrbit(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| computeJacobianMeanWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| FieldKeplerianOrbit(Field, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPerigeeArgumentDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRightAscensionOfAscendingNodeDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTrueAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTrueAnomalyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |